Investigation of linear plug layouts of rocket engines for reusable launch vehicles

36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2000, Pages

  Duranov, G E ^a   Klimov, V V ^a   Ponomarev, N B ^a  

^a KELDYSH RESEARCH CENTER   (Russian Federation)

Author keywords

[No Author keywords available]

Indexed keywords

OPTIMIZATION; PROPULSION; ROCKET ENGINES;

BASE PRESSURE; COMPUTATIONAL ANALYSIS; EXPERIMENTAL INVESTIGATIONS; PLUG NOZZLE; PRIMARY NOZZLES; REUSABLE LAUNCH VEHICLES; THRUST LOSS; WALL-PRESSURE DISTRIBUTION;

NOZZLES;

EID: 85081809964     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. Beichel, R., Nozzle Concepts for Single-Stage Shuttles, Astronautics & Aeronautics, v.14, No.6, June 1975.
2. Kirby, F.M. and Martinez, A., Linear Aerospike Engine, AIAA Paper 77-968.
3. Vinson, J., Aerospike Engine Design Gains New Thrust, Aerospace America, Feb., 1998.
4. Immich, H., Nasuti, F., Onofri, M., and Caporicci, M., Experimental and Numerical Analysis of Linear Plug Nozzles, AIAA Paper 98-1603.
5. Pirumov, U.G., Roslyakov, G.S., Gas Dynamics of Nozzles, M., "Nauka", 1990 (in Russian).
6. Ponomarev, N.B., Program Package for Computation of Two-Dimensional Ideal Gas Flow in Nozzles - PEGAS. State Fund of Algorithms and Programs, No. S00053, 1985 (in Russian).
7. Ponomarev, N.B., Direct Optimization of Rocket Engine Nozzle Contours. In: "Space-Rocket Technique: Rocket Engines and Power Plants", Keldysh Research Center, issue 2(135), 1992 (in Russian).